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JP4402252B2 - Three-dimensional woven braid for composite materials and composite materials - Google Patents
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JP4402252B2 - Three-dimensional woven braid for composite materials and composite materials - Google Patents

Three-dimensional woven braid for composite materials and composite materials Download PDF

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Publication number
JP4402252B2
JP4402252B2 JP2000122264A JP2000122264A JP4402252B2 JP 4402252 B2 JP4402252 B2 JP 4402252B2 JP 2000122264 A JP2000122264 A JP 2000122264A JP 2000122264 A JP2000122264 A JP 2000122264A JP 4402252 B2 JP4402252 B2 JP 4402252B2
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Japan
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fiber
dimensional
dimensional woven
woven braid
composite material
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JP2000122264A
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JP2001303385A (en
Inventor
雅弘 新屋
西山  茂
豊己 田中
裕之 桐山
和民 三谷
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Mitsubishi Chemical Corp
Mitsubishi Heavy Industries Ltd
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Mitsubishi Chemical Corp
Mitsubishi Heavy Industries Ltd
Mitsubishi Rayon Co Ltd
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Description

【0001】
【発明の属する技術分野】
本発明は、形状が複雑な繊維強化樹脂系複合材料製品(以下、本明細書では繊維強化複合材製品という)を低コストで製造するための複合材料の繊維素材及び構造部品に関する。
【0002】
【従来の技術】
軽量で強靱な強度を有し、しかも複雑な形状にされた繊維強化複合材製品の製造に当っては、一般的に、連続繊維を一方向に並べたり、織り上げた物に半硬化状態の樹脂を塗りつけてシート状にした素材であるプリプレグを、製造する製品形状に合せて積み重ねて製作することが行われている。
この場合、プリプレグ中に途中で切断されてない真直ぐな連続繊維がある場合、当該連続繊維に沿った方向について、特に、優れた力学的強度が得られる反面、プリプレグを積み重ねて製作される製品の厚み方向の力学的強度は、プリプレグを構成する樹脂の結合力のみに依存する場合が多く、このため、一般に厚み方向の力学的強度は強化繊維で補強された板内方向に比して小さい。
【0003】
このような不具合を解消し、製品の厚み方向の力学的強度を向上させるために、プリプレグの表層に熱可塑性樹脂を混在させて、この熱可塑性樹脂の結合力で厚み方向の素材間の力学的強度、すなわち、繊維強化複合材製品の破壊のしにくさである、靱性を向上させることも提案されている。
例えば、特開平1−110537号「球状微粒子を有するプリプレグ」では、プリプレグの表層に、球状の熱可塑性樹脂の微粒子を、プリプレグで形成されている各層の厚みの表面から30%以内の深さに局在化させることにより、プリプレグシート間の接合面の靱性を効果的に向上させ、シート状素材の接合面における破壊強度を大きくして、高強度の繊維強化複合材製品を製作するものが開示されている。
【0004】
しかしながら、プリプレグで複雑な立体形状の製品を製作するには、プリプレグを所要寸法に切り出して、製品形状を単純形状要素に分割した要素毎の形状に積み重ねるレイアップ作業や、重ね合わせたプリプレグの間に取り込まれた空気を吸い出したりするデバルク作業等の予備成形工程を実施する必要があり、さらには、これらの単純形状要素を製品の最終的な立体形状に組み上げた後においても、同様な作業を必要とし、製品製作工程数の増加をきたし、より多くの作業時間や手間を要し、製品の製造コストが嵩むという不具合がある。
【0005】
一方、シート状素材の積層により成形した繊維強化複合材製品が厚み方向の強度を発現し難いことを克服するために、厚み方向を含めた立体的な方向に、連続繊維を立体的に絡め合わせて製品形状に織編組製した繊維組織を樹脂で固めて、繊維複合材製品を製造して、厚み方向の力学的強度をも補強するようにした三次元複合材の開発が進められている。
しかしながら、このような三次元複合材にして、何れの方向の力学的強度に対しても補強を行い、秀れた強度を有する繊維複合材製品にするためには、特に、繊維強化複合材製品が複雑な形状をしている場合において、連続繊維を製品形状に合せて立体的な繊維組織に織編組製するための専用の道具、設備を必要とし、さらには、複雑な形状の繊維複合材製品に対応した立体的繊維組織を織編組製するためには、多数の時間や手間を要し、プリプレグの場合と同様、製造コストが高くなるという不具合がある。
複雑な立体的製品形状を、単純な形状要素に分割して、それぞれを厚み方向にも補強繊維が配列されるよう三次元的に織編組製した織編組物となし、その織編組物を製品の最終的な立体形状に組み上げて樹脂で固めることも可能であるが、この場合、要素とした織編組物間の力学的強度は、樹脂の結合力のみに依存するので、強化繊維で補強された部分の強度に比べて低くなるのが一般的である。
【0006】
【発明が解決しようとする課題】
本発明は、複雑な立体形状をした繊維強化複合材製品の製造において、従来から採用されている製品製造方法において生じている不具合を解消するために、繊維強化複合材製品の単純形状要素毎の、プリプレグの切り出し、要素毎の形状に積み重ねるレイアップ作業、積み重ねられたプリプレグの接合間毎の空気を吸い出すデバルク作業等の予備成形工程を必要とせず、あるいは、複雑な製品形状の繊維強化複合材製品に合せた立体的形状にするための連続繊維を織編組製するための専用の道具や設備を必要とせず、また、織編組製するための時間や手間が少なく、しかも、繊維素材間にも充分な強度を有する、複雑な形状の繊維強化複合材製品を安価に製造できる複合材料用三次元織編組物、及び、この織編組物を用いて形成される構造部品を提供することを課題とする。
【0007】
【課題を解決するための手段】
このため、本発明の複合材料の繊維素材は次の手段を採用した。
【0008】
(1)弾性強度の大きい強化繊維からなる複合材料用三次元織編組物であって、弾性強度は強化繊維に劣るものの、一体成形時に樹脂との結合力が大きく、強化繊維と一体となって靱性を向上させ、破壊強度を増加させる結合力向上繊維が複合化された複合材料用三次元織編組物。なお、本発明において、強化繊維からなる複合材料用三次元織編組物であって、結合力向上繊維が複合化された織編組物とは三次元織物にした強化繊維に結合力向上繊維を織り込んだ織物にしたもの、又は強化繊維を三次元編物にした強化繊維に結合力向上繊維を編み込んだ編物にしたもの、あるいは三次元組物にした強化繊維に結合力向上繊維を組み込んだ組物にしたもの、それぞれの織物、編物、あるいは組物と同等の組織を有する強化繊維と結合力向上繊維の集合体を意味し、強化繊維の糸条と結合力向上繊維の糸条を独立の糸条として同時に織編組製する、強化繊維の糸条の織編組物に結合力向上繊維を追加する、あるいは強化繊維と結合力向上繊維の糸条を引き揃えもしくは撚り合わせる等した糸条を用いて織編組製する等の、種々の織編組製手順を用いることが可能であり、織編組製の手順は問わない。
また、前記結合力向上繊維が、繊維素材各部位の厚みにおいて表面から厚みの1/4深度まで、もしくは表面から0.5mm深さまでのいずれか小さい方の深さの空間における結合力向上繊維の体積占有率が、繊維素材のその他の部分における結合力向上繊維の体積占有率よりも大きい状態とした。
【0009】
(a)本発明の複合材料用三次元織編組物は、上述(1)の手段にしたことにより、従来プリプレグの予備成形工程において必要とされていた、繊維強化複合材製品形状を単純形状要素に分割し、要素毎の形状に合せてプリプレグを所要寸法に切り出して積み重ねるレイアップ作業や、所定数毎のレイアップ作業毎に行われる重ね合わせたプリプレグの間の樹脂に取り込まれている空気を吸い出すデバルグ作業等の予備成形工程における作業を不要とし、強化繊維と結合力向上繊維とを織編組製した単純形状の織編組物を、製品形状に組み上げた後の、樹脂の含浸および硬化作業、いわゆる、成形作業だけで製品形状の繊維強化複合材料が得られるため、製品製作工程数が低減し、作業時間や手間を少くでき、製造コストを低減する。
また、立体的な繊維強化複合材製品を形成するために組み合わせる織編組物間ならびに繊維素材間近傍において、結合力向上繊維を特に多く配置する事が可能となり、効果的に織編組物間の靱性を向上することができる。
【0010】
また、本発明の複合材料用三次元織編組物は、上述(1)の手段に加え、次の手段を採用した。
【0011】
(2)強化繊維は弾性率200GPa以上の高弾性繊維であり、結合力向上繊維は弾性率100GPa以下の繊維状熱可塑性樹脂からなり、成形された繊維強化複合材製品の複合材料用三次元織編組物間の破壊強度を向上させるものとした。
【0012】
(b)本発明の複合材料用三次元織編組物は、上述(2)の手段にしたことにより、上述(a)に加え、このような複合材料用三次元織編組物で形成された繊維強化複合材製品は、強度的に航空宇宙分野、船舶、スポーツ用品、および建築物の材料として好適な破壊強度等の材料特性を具えるものとすることができ、特に、軽量化が要求される航空宇宙分野に使用される製品には、大幅な軽量化が図れる材料特性を具えることから、これらの織編組物を繊維強化複合材製品に採用し製作された航空機宇宙機器等の性能向上に寄与することができる。
【0013】
また、本発明の複合材料用三次元織編組物は、上述(1)の手段又は上述(1)の手段および(2)の手段とを具えたものに加え、次の手段を採用した。
【0014】
(3)強化繊維は樹脂未含浸の炭素繊維、アラミド繊維若しくはガラス繊維のいずれか1つ若しくはそれらの組み合わせからなり、また、結合力向上繊維はポリアミド、ポリエステル、ポリエーテルエーテルケトン、ポリエーテルイミド若しくはポリイミドのいずれか1つ若しくはそれらの組合わせからなる熱可塑性樹脂を繊維状にしたものとした。
【0015】
(c)本発明の複合材料用三次元織編組物は、上述(3)の手段にしたことにより、上述(a)又は上述(a),(b)に加え、立体的な繊維強化複合材製品を形成する織編組物において、高強度、高弾性繊維である炭素繊維、ガラス繊維、あるいはアラミド繊維からなり、構成部材の高強度、高弾性向上に効果を発揮し、繊維強化複合材製品の構造強度及び弾性を向上させることができる。
【0016】
また、強化繊維の組織中に、ポリアミド、ポリエステル、ポリエーテルエーテルケトン、ポリエーテルイミド、あるいはポリイミドからなる熱可塑性樹脂で形成された結合力向上繊維が織り込まれ、若しくは編み込まれ、若しくは組み込まれて、繊維素材同士の接合面における靱性強度が向上し、繊維強化複合材製品を形成する構造部品の破壊強度を向上させることができ、特に、組み合わせて繊維強化複合材製品を形成する構造部品である織編組物間の接合面の破壊強度を向上させることができ、これらの複合材料用三次元織編組物を組み合わせて成形された繊維強化複合材製品の靱性強度を向上させ、破壊強度を向上させることができる。
【0017】
さらに、繊維強化複合材製品を一体的に製作するとき、必要とする形状要素毎にプリプレグを所要の寸法に切り出し、製作形状に合わせて積み重ねるレイアップ作業及び積み重ねたプリプレグ間の空気を抜き出すデバルグ作業が不要になり、安価な製造コストで、特に、形状が複雑な立体形状の繊維強化複合材製品を形成することができる。
【0021】
)さらに、本発明の上述(1)の手段又は上述(1),(2)の手段又は上述(1),(2),(3)の手段にした複合材料用三次元織編組物を使用して、形成する複合材料は、次の手段を採用した。強化繊維と結合力向上繊維とを複合化した複数の単純形状の三次元織編組物を、所望の立体形状を呈するように組み合わせた後、立体形状に組み合わされている強化繊維と結合向上繊維とからなる複合材料用織編組物に、樹脂を含浸させて成形するものとした。
【0022】
)本発明の複合材料は、上述()の手段により成形するようにしたことにより、強化繊維と結合力向上繊維とを複合化した三次元織編組物を用いることにより、製品形状に組み合わせた後、樹脂で固めることにより、繊維強化複合材製品に形成された織編組物の接合面における靱性強度が向上し、繊維強化複合材製品の破壊強度を向上させることができる。
【0023】
さらに、シート状素材で複雑形状の繊維強化複合材製品を製作するときに必要としていた、形状要素毎にシート状素材を所要の寸法に切り出して、製作形状に合わせて積み重ねるレイアップ作業や、シート状素材を所定数積み重ねる毎に行う必要のあったシート状素材間の空気を抜き出すデバルク作業等の予備成形工程作業が不要になり、安価な製造コストで、形状が複雑な立体形状の繊維強化複合材製品を形成でき、複合材料とすることができる。
【0024】
一方、強化繊維と結合力向上繊維とを複合化した複数の簡素な形状にされた三次元織編組物を、所望の立体形状を呈するよう組み合わせて、繊維強化複合材製品が製作されるので、特に、複雑な形状の繊維強化複合材製品を製作する場合において、複雑な三次元形状の繊維強化複合材製品に対応した立体的繊維組織を織編組製するために、従来必要としていた専用道具、設備が不要になるとともに、織編組製等に要する時間および手間を少なくでき、安価な製造コストで、特に、形状が複雑な立体形状の繊維強化複合材製品の場合でも、短時間でしかも容易に形成できる複合材料とすることができる。
【0025】
【発明の実施の形態】
以下、本発明の複合材料用三次元織編組物及び複合材料の実施の一形態を図面にもとづき説明する。
【0026】
図1は本発明の複合材料用三次元織編組物の実施例で、第1形態として三次元織物を示す斜視図である。
図において、1は強化繊維で複合材料の強化材(Reinforcement)を構成する部分であり、炭素繊維、ガラス繊維あるいはアラミド繊維等の高強度、高弾性の素材の何れか、若しくはこれらの素材を組合せて形成された繊維である。
2は結合力向上繊維で、ポリアミド、ポリエステル、ポリエーテルエーテルケトン、ポリエーテルイミドあるいはポリイミドの何れかの熱可塑性樹脂等の靱性向上効果のある素材で形成された繊維である。
【0027】
上述した、強化繊維1、結合力向上繊維2により、三次元織物10aに形成された複合材料用三次元織物を、製品の形状に組み合わせた後、樹脂(基材:マトリックス)で1度に固めることにより、素材間がより強固に結合された高強度で破壊強度の大きい繊維強化複合材製品を成形することができる。
【0028】
以上、三次元織物を例にして示したが、三次元編物又は三次元組物として構成することもできる。織編組物の形態や組織は、安価で構成する事が可能なものであれば、その種類は問わないものである。
例えば、本出願人等が、特開平10−325041号「三次元繊維」で提案した、安価で高性能複合材製品向けの繊維組織の構成が可能な織機より織製される三次元織物を使用するようにしても良いものである。
【0029】
強化繊維の三次元織編組物の組織内部へ結合力向上繊維を複合化した場合、素材同士の結合面のみならず、素材内部の靱性向上効果も得られ、これらの素材を用いて製作された複合材製品全体を破壊強度に優れたものにすることもできる。さらに、特に、繊維強化複合材製品が複雑な形状をしている場合において、従来技術で必要であった、繊維強化複合材製品形状を単純形状要素に分割し、要素毎に行われるレイアップ作業や、デバルク作業等の予備成形工程を実施することが不要になり、さらには、これらの単純形状要素を製品形状に組み上げた後において行われる成形作業だけとなるために、製品製作工程数の増加に伴う時間や手間が不要になり、製品の製造コストが低減できる。
【0030】
あるいは、連続繊維を製品形状に合せて立体的な繊維組織を織編組製する方法に比べても、専用の道具設備が不要になり、さらには、織編組製するための多数の時間がかからず、同様に製造コストが低減できるという利点がある。
【0031】
次に、上述の構成にした本実施の第1形態の複合材料用三次元織物10a間の補強効果を確認する為、台座部5と突起部6間の接合面剥離強度試験を実施した結果について説明する。
【0032】
図2は、この剥離強度試験の原理を示す図である。
図に示すように、剥離強度試験に使用される供試材料7には、前述した5軸三次元織物を長さ200m/m、幅50m/m、厚み1.2m/mに切り出した台座部5に長さ70m/m、幅50m/m、厚み1.2m/mに切り出した突起部6を2枚積み重ね、一度に樹脂で固めた(複合材成形した)ものを用い、5軸三次元織物表面に結合力向上繊維2を挟んだものと、はさまないものの2種類の供試材料7を準備した。
【0033】
試験は、図に示すように供試材料7の台座部5に設けた支持点11で支持した後、反対側の中心から15m/m離隔した位置に設けた負荷点8より荷重9を加え、台座部5から突起部6が剥がれる最大荷重9max を剥離強度として計測することとした。
【0034】
この結果、図3に示すように、台座部5と突起部6との間に結合力向上繊維2としてのポリイミドファイバ繊維をはさみ込まなかった場合の最大荷重9max は、約31kgfであったものが、ポリイミドファイバ繊維を組込んだ場合には、約35kgfにまで大きくなり、最大荷重9max は約13%向上することが判った。
【0035】
【発明の効果】
以上説明したように、本発明の複合材料用三次元織編組物は、高強度、高弾性の強化繊維と、繊維強化複合材製品の破壊強度を向上させる結合力向上繊維を、複合化して織編組製されるものとした。
これにより、複合材料用三次元織編組物同士を組合わせて形成する構造部品の接合面の相互結合が補強され、繊維強化複合材製品の破壊強度を向上することができる。
【0036】
さらに、複雑な立体形状の繊維強化複合材製品を成形するときの単純形状要素毎にプリプレグを所要の寸法に切り出して積み重ねる作業、所定数積み重ねたシート状素材間の空気の抜き出し作業等の予備成形工程が不要になり、安価な製造コストで形状が複雑な立体形状の繊維強化複合材製品を形成できる。
【図面の簡単な説明】
【図1】本発明の複合材料用三次元織編組物の実施例の第1形態としての三次元織物を示す斜視図、
【図2】図1に示す複合材料用三次元織物の剥離強度試験の原理を示す模式図、
【図3】図2に示す剥離強度試験でなされた試験結果を示す図である。
【符号の説明】
1 強化繊維
2 結合力向上繊維
5 台座部
6 突起部
7 供試材料
8 負荷点
9 荷重
10a 三次元織物
11 支持点
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a fiber material and a structural component of a composite material for manufacturing a fiber reinforced resin composite material product having a complicated shape (hereinafter referred to as a fiber reinforced composite material product) at low cost.
[0002]
[Prior art]
In the manufacture of fiber reinforced composite products that are lightweight and tough and have a complex shape, generally, a continuous-type fiber is arranged in one direction, or a semi-cured resin in a woven product. A prepreg, which is a material formed by applying a sheet to form a sheet, is stacked and manufactured according to the shape of the product to be manufactured.
In this case, when there is a straight continuous fiber that is not cut in the middle of the prepreg, particularly in the direction along the continuous fiber, particularly excellent mechanical strength can be obtained, but the product manufactured by stacking the prepregs. The mechanical strength in the thickness direction often depends only on the bonding force of the resin constituting the prepreg, and therefore the mechanical strength in the thickness direction is generally smaller than the in-plate direction reinforced with reinforcing fibers.
[0003]
In order to eliminate such problems and improve the mechanical strength in the thickness direction of the product, a thermoplastic resin is mixed in the surface layer of the prepreg, and the mechanical strength between the materials in the thickness direction is determined by the bonding force of this thermoplastic resin. It has also been proposed to improve strength, that is, toughness, which is the difficulty of breaking fiber reinforced composite products.
For example, in Japanese Patent Application Laid-Open No. 1-110537 “prepreg having spherical fine particles”, spherical thermoplastic resin fine particles are formed on the surface layer of the prepreg within a depth of 30% from the surface of the thickness of each layer formed of the prepreg. Disclosed is to produce a high-strength fiber-reinforced composite product by effectively improving the toughness of the joint surface between prepreg sheets by increasing the localization, increasing the fracture strength at the joint surface of the sheet-like material Has been.
[0004]
However, in order to manufacture products with complicated three-dimensional shapes using prepreg, prepreg is cut out to the required dimensions, and the product shape is divided into simple shape elements and stacked into individual element shapes. It is necessary to perform a preforming process such as a debulk operation that sucks out the air taken in, and even after these simple shape elements are assembled into the final three-dimensional shape of the product, the same operation is performed. This increases the number of product manufacturing steps, requires more work time and labor, and increases the manufacturing cost of the product.
[0005]
On the other hand, continuous fibers are entangled three-dimensionally in three-dimensional directions including the thickness direction in order to overcome the difficulty of developing strength in the thickness direction of fiber-reinforced composite products formed by laminating sheet-like materials. Development of a three-dimensional composite material in which the fiber structure woven and braided into a product shape is solidified with a resin to produce a fiber composite product to reinforce the mechanical strength in the thickness direction is also underway.
However, in order to make such a three-dimensional composite material to reinforce the mechanical strength in any direction and to make a fiber composite product having excellent strength, in particular, a fiber reinforced composite product Requires a dedicated tool and equipment for weaving and braiding a continuous fiber into a three-dimensional fiber structure in accordance with the product shape, and a complex composite fiber composite material. In order to fabricate and fabricate a three-dimensional fiber structure corresponding to a product, a lot of time and labor are required, and there is a problem that the manufacturing cost becomes high as in the case of a prepreg.
A complicated three-dimensional product shape is divided into simple shape elements, and each is formed into a woven braid that is woven and braided three-dimensionally so that the reinforcing fibers are arranged in the thickness direction. However, in this case, the mechanical strength between the woven and braided elements used as the element depends only on the bonding strength of the resin, so it is reinforced with reinforcing fibers. In general, it is lower than the strength of the part.
[0006]
[Problems to be solved by the invention]
In the production of a fiber reinforced composite product having a complicated three-dimensional shape, the present invention eliminates the problems that have occurred in the product manufacturing method that has been conventionally employed. , Prepreg cutting, lay-up work for stacking in the shape of each element, debulking work for sucking out air for each joint of stacked prepregs, etc. There is no need for special tools and equipment for producing woven braided continuous fibers to make a three-dimensional shape that matches the product, and less time and labor for woven braided production. Three-dimensional woven braid for composite materials that can be manufactured at low cost with a complex shape fiber reinforced composite material having sufficient strength, and a structure formed using the woven braid It is an object of the present invention to provide a.
[0007]
[Means for Solving the Problems]
For this reason, the following means was employ | adopted for the fiber raw material of the composite material of this invention.
[0008]
(1) A three-dimensional woven braid for composite materials composed of reinforcing fibers with high elastic strength, which is inferior to reinforcing fibers, but has a high binding force with the resin during integral molding, and is integrated with the reinforcing fibers. A three-dimensional woven braid for composite materials in which fibers with improved binding strength that improve toughness and fracture strength are combined. In the present invention, a three-dimensional woven braid for composite materials composed of reinforcing fibers, in which a binding strength improving fiber is compounded, is a three-dimensional woven fiber woven with a binding strength improving fiber. A woven fabric, a knitted fabric in which a reinforcing fiber is knitted with a reinforcing fiber in a three-dimensional knitted fabric, or a knitted fabric in which a binding strength improving fiber is incorporated in a reinforced fiber in a three-dimensional braid. , Woven fabrics, knitted fabrics or aggregates of reinforcing fibers having the same structure as the braids, and the binding strength improving fibers, and the reinforcing fibers and the binding strength improving yarns are independent yarns. Weaving using yarns that are made simultaneously, such as woven braids, adding reinforcing fibers to the woven braids of reinforcing fiber yarns, or aligning or twisting the reinforcing fiber and binding fiber yarns together Seeds, such as braided Of the use of a woven braid made steps are possible, the procedure of weaving the braid does not matter.
In addition, the binding strength improving fiber is a thickness of each part of the fiber material, from the surface to 1/4 depth of the thickness, or from the surface to the depth of 0.5 mm, whichever is the smaller depth space of the binding strength improving fiber The volume occupancy was set to be greater than the volume occupancy of the binding force improving fibers in the other portions of the fiber material.
[0009]
(A) The three-dimensional woven braid for composite material according to the present invention has the shape of the fiber reinforced composite material product, which has been conventionally required in the preforming step of the prepreg, by using the means of (1) above. The air that is taken into the resin between the prepregs that are divided into two, layup work that cuts and stacks the prepreg according to the shape of each element and stacks each predetermined number of layup work Impregnation and curing work of resin after assembling a simple shape woven braid into a product shape, which eliminates the need for work in the preforming process such as debulking work to suck out, and woven and braided reinforcing fibers and binding strength improving fibers, Since a fiber-reinforced composite material having a product shape can be obtained only by a so-called molding operation, the number of product manufacturing steps can be reduced, working time and labor can be reduced, and manufacturing costs can be reduced.
In addition, it is possible to place particularly many fibers with improved binding strength between the woven braids combined to form a three-dimensional fiber-reinforced composite material product and in the vicinity of the fiber materials. Can be improved.
[0010]
Moreover, the three-dimensional woven braid for composite material of the present invention employs the following means in addition to the above-mentioned means (1).
[0011]
(2) Reinforcing fiber is a high elastic fiber having an elastic modulus of 200 GPa or more, and the binding strength improving fiber is made of a fibrous thermoplastic resin having an elastic modulus of 100 GPa or less. The fracture strength between the braids was improved.
[0012]
(B) The three-dimensional woven braid for composite material according to the present invention is a fiber formed of such a three-dimensional woven braid for composite material in addition to the above (a) by adopting the means of (2) above. Reinforced composite products can have material properties such as breaking strength that are suitable as materials for aerospace, ship, sporting goods, and building in terms of strength, and in particular, weight reduction is required. Products used in the aerospace field have material characteristics that can be significantly reduced in weight, so these woven braids are used in fiber reinforced composite products to improve the performance of aircraft and space equipment manufactured. Can contribute.
[0013]
The three-dimensional woven braid for composite material of the present invention employs the following means in addition to the means (1) or the means (1) and (2).
[0014]
(3) The reinforcing fiber is made of any one of carbon fiber, aramid fiber or glass fiber which is not impregnated with resin or a combination thereof, and the bonding strength improving fiber is polyamide, polyester, polyetheretherketone, polyetherimide or A thermoplastic resin made of any one of polyimides or a combination thereof was made into a fibrous form.
[0015]
(C) The three-dimensional woven braid for composite material according to the present invention is a three-dimensional fiber-reinforced composite material in addition to the above-mentioned (a) or the above-mentioned (a), (b) by using the above-mentioned means (3). The woven braid that forms a product is made of carbon fiber, glass fiber, or aramid fiber, which are high-strength and high-elasticity fibers, and is effective in improving the high-strength and high-elasticity of components. Structural strength and elasticity can be improved.
[0016]
In addition, in the structure of the reinforcing fiber, a bonding strength improving fiber formed of a thermoplastic resin composed of polyamide, polyester, polyetheretherketone, polyetherimide, or polyimide is woven, knitted, or incorporated, The toughness strength at the joint surface between fiber materials can be improved, and the fracture strength of structural parts forming fiber reinforced composite products can be improved. The fracture strength of the joint surface between braids can be improved, and the toughness and strength of fiber reinforced composite products formed by combining these three-dimensional woven braids for composite materials can be improved. Can do.
[0017]
Furthermore, when manufacturing fiber reinforced composite products as a single unit, prepregs are cut out to the required dimensions for each required shape element, stacked in accordance with the manufacturing shape, and debulking operations to extract air between the stacked prepregs. Can be formed, and a three-dimensional fiber-reinforced composite material product having a particularly complicated shape can be formed at a low manufacturing cost.
[0021]
(4) In addition, means or above the above-mentioned (1) of the present invention (1), (2) means or above (1), (2), the composite material for three-dimensional woven braid you means (3) The following means was adopted for the composite material to be formed. After combining a plurality of simple-shaped three-dimensional woven braids obtained by combining reinforcing fibers and bonding strength improving fibers so as to exhibit a desired three-dimensional shape, the reinforcing fibers combined with the three-dimensional shape and the bonding improving fibers A woven braid for composite material made of is impregnated with a resin and molded.
[0022]
( D ) The composite material of the present invention is formed into a product shape by using a three-dimensional woven braid in which reinforcing fibers and binding strength improving fibers are composited by being molded by the means of ( 4 ) above. After combining, by hardening with resin, the toughness strength at the joint surface of the woven braid formed in the fiber reinforced composite product can be improved, and the fracture strength of the fiber reinforced composite product can be improved.
[0023]
In addition, lay-up work that cuts sheet-like materials into the required dimensions for each shape element and stacks them according to the production shape, which was necessary when manufacturing fiber-reinforced composite products with complex shapes using sheet-like materials, and sheets This eliminates the need for pre-molding processes such as debulking to extract air between sheet-shaped materials each time a predetermined number of sheet-shaped materials are stacked, making it a low-cost manufacturing cost and a three-dimensional fiber-reinforced composite with a complicated shape. A material product can be formed and can be a composite material.
[0024]
On the other hand, since a fiber-reinforced composite material product is manufactured by combining a plurality of simple three-dimensional woven braids obtained by combining reinforcing fibers and binding strength improving fibers so as to exhibit a desired three-dimensional shape, In particular, in the case of producing a fiber reinforced composite product having a complicated shape, a dedicated tool that has been conventionally required to produce a three-dimensional fiber structure corresponding to the fiber reinforced composite product having a complicated three-dimensional shape, Equipment is not required, and the time and labor required for weaving and braiding can be reduced, and at low cost, especially in the case of complex-shaped three-dimensional fiber reinforced composite products, in a short time and easily. It can be a composite material that can be formed.
[0025]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, one embodiment of a three-dimensional woven braid for composite materials and a composite material of the present invention will be described with reference to the drawings.
[0026]
FIG. 1 is a perspective view showing a three-dimensional woven fabric as a first embodiment in an embodiment of a three-dimensional woven braid for composite material of the present invention.
In the figure, reference numeral 1 is a portion constituting a reinforcing material (Reinforcement) of a composite material with reinforcing fibers, and is one of high-strength and high-elastic materials such as carbon fiber, glass fiber or aramid fiber, or a combination of these materials. It is a fiber formed.
Reference numeral 2 denotes a binding strength improving fiber, which is a fiber formed of a material having an effect of improving toughness such as a thermoplastic resin such as polyamide, polyester, polyether ether ketone, polyether imide, or polyimide.
[0027]
After combining the three-dimensional fabric for composite material formed in the three-dimensional fabric 10a with the reinforcing fiber 1 and the binding strength improving fiber 2 described above into the shape of the product, the resin (base material: matrix) is solidified at once. As a result, a fiber-reinforced composite material product having high strength and high breaking strength in which the materials are more firmly bonded can be formed.
[0028]
As described above, the three-dimensional woven fabric is shown as an example. However, it can be configured as a three-dimensional knitted fabric or a three-dimensional braid. The form and structure of the woven braid are not limited as long as it can be constructed at low cost.
For example, a three-dimensional woven fabric woven from a loom capable of forming a fiber structure for an inexpensive and high-performance composite material proposed by the present applicants in Japanese Patent Laid-Open No. 10-325041 “Three-dimensional fiber” is used. It may be made to do.
[0029]
When fibers with improved binding strength are combined inside the structure of a three-dimensional woven braid of reinforcing fibers, not only the bonding surfaces of the materials but also the effect of improving the toughness inside the materials can be obtained. It is also possible to make the entire composite product excellent in breaking strength. Furthermore, especially when the fiber-reinforced composite product has a complex shape, the fiber-reinforced composite product shape required for the prior art is divided into simple-shaped elements, and the lay-up work performed for each element. In addition, it is no longer necessary to perform a pre-molding process such as debulk work, and moreover, the number of product manufacturing processes is increased because only these molding operations are performed after assembling these simple shape elements into a product shape. This eliminates the time and labor involved in reducing the manufacturing cost of the product.
[0030]
Or, compared to the method of weaving and braiding a three-dimensional fiber structure by matching the continuous fiber to the product shape, no dedicated tool equipment is required, and more time is required for making the weaving braid. Similarly, there is an advantage that the manufacturing cost can be reduced.
[0031]
Next, in order to confirm the reinforcing effect between the three-dimensional woven fabric 10a for composite materials according to the first embodiment having the above-described configuration, the results of the joint surface peel strength test between the pedestal portion 5 and the protrusion 6 are performed. explain.
[0032]
FIG. 2 is a diagram showing the principle of this peel strength test.
As shown in the figure, the test material 7 used for the peel strength test is a pedestal part obtained by cutting the above-described 5-axis three-dimensional fabric into a length of 200 m / m, a width of 50 m / m, and a thickness of 1.2 m / m. 5-axis, three-dimensional, using two protrusions 6 cut into a length of 70 m / m, a width of 50 m / m, and a thickness of 1.2 m / m, and solidified with resin at one time (molded with a composite material) Two types of test materials 7 were prepared, one having the bonding strength improving fiber 2 sandwiched between the fabric surfaces and the other having no sandwich.
[0033]
As shown in the figure, the test was supported at a support point 11 provided on the pedestal 5 of the test material 7, and then a load 9 was applied from a load point 8 provided at a position 15 m / m away from the opposite center, The maximum load 9 max at which the protrusion 6 is peeled off from the pedestal 5 is measured as the peel strength.
[0034]
As a result, as shown in FIG. 3, the maximum load 9 max when the polyimide fiber fiber as the bonding strength improving fiber 2 is not sandwiched between the pedestal portion 5 and the protruding portion 6 is about 31 kgf. However, it was found that when the polyimide fiber fiber was incorporated, it increased to about 35 kgf and the maximum load 9 max was improved by about 13%.
[0035]
【The invention's effect】
As described above, the three-dimensional woven braid for composite material according to the present invention is a woven material obtained by combining high-strength, high-elasticity reinforcing fibers and bonding strength improving fibers that improve the breaking strength of fiber-reinforced composite products. It was supposed to be braided.
Thereby, the mutual coupling | bonding of the joint surface of the structural components formed combining three-dimensional woven braids for composite materials is reinforced, and the fracture strength of a fiber reinforced composite material product can be improved.
[0036]
Furthermore, when molding complex three-dimensional fiber reinforced composite products, pre-forms such as cutting out prepregs for each simple shape element and stacking them up, stacking a predetermined number of sheets, extracting air between sheets, etc. A process is not required, and a three-dimensional fiber-reinforced composite material product having a complicated shape can be formed at a low manufacturing cost.
[Brief description of the drawings]
FIG. 1 is a perspective view showing a three-dimensional woven fabric as a first form of an embodiment of a three-dimensional woven braid for composite material of the present invention;
FIG. 2 is a schematic diagram showing the principle of a peel strength test of the three-dimensional fabric for composite material shown in FIG.
FIG. 3 is a diagram showing test results obtained in the peel strength test shown in FIG. 2;
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Reinforcement fiber 2 Bonding power improvement fiber 5 Base part 6 Protrusion part 7 Test material 8 Load point 9 Load 10a Three-dimensional fabric 11 Support point

Claims (4)

強化繊維からなる複合材料用三次元織編組物であって、前記強化繊維と比較して前記複合材料用三次元織編組物と一体成形される樹脂との結合力が大きい結合力向上繊維が複合化され、前記複合材料用三次元織編組物の各部位の繊維素材各部位の厚みにおいて表面から厚みの1/4深度まで、もしくは表面から0.5mm深さまでのいずれか小さい方の深さの空間における、前記結合力向上繊維の体積占有率が、複合材料用三次元織編組物のその他の部分における結合力向上繊維の体積占有率よりも大きい複合材料用三次元織編組物。A three-dimensional woven braid for composite materials composed of reinforcing fibers, which is combined with a binding strength improving fiber that has a greater binding strength with the resin integrally molded with the three-dimensional woven braid for composite materials than the reinforcing fibers. The thickness of each part of the fiber material of each part of the three-dimensional woven braid for composite material is from the surface to a depth of 1/4 of the thickness or from the surface to a depth of 0.5 mm, whichever is smaller The three-dimensional woven braid for composite materials, wherein the volume occupancy of the binding force improving fibers in the space is larger than the volume occupancy of the binding strength improving fibers in other parts of the three-dimensional woven braid for composite materials. 前記強化繊維は弾性率200GPa以上の繊維であり、前記結合力向上繊維は弾性率100GPa以下の繊維状熱可塑性樹脂であることを特徴とする請求項1の複合材料用三次元織編組物。  The three-dimensional woven braid for composite material according to claim 1, wherein the reinforcing fiber is a fiber having an elastic modulus of 200 GPa or more, and the binding force improving fiber is a fibrous thermoplastic resin having an elastic modulus of 100 GPa or less. 前記強化繊維は炭素繊維、アラミド繊維若しくはガラス繊維のいずれか1つ若しくはそれらを組み合わせたものであり、前記結合力向上繊維はポリアミド、ポリエステル、ポリエーテルエーテルケトン、ポリエーテルイミド若しくはポリイミドのいずれか1つ若しくはそれらの組合わせからなる熱可塑性樹脂を繊維状にしたものであることを特徴とする請求項1又は2の複合材料用三次元織編組物。  The reinforcing fiber is any one of carbon fiber, aramid fiber, glass fiber, or a combination thereof, and the bonding strength improving fiber is any one of polyamide, polyester, polyetheretherketone, polyetherimide, or polyimide. The three-dimensional woven braid for composite materials according to claim 1 or 2, wherein a thermoplastic resin comprising one or a combination thereof is made into a fiber. 請求項1から3のいずれか1項記載の複合材料用三次元織編組物を、所望の製品形状に組み合わせた状態で、樹脂を含浸硬化した繊維強化複合材料。A fiber-reinforced composite material obtained by impregnating and curing a resin in a state where the three-dimensional woven braid for composite material according to any one of claims 1 to 3 is combined in a desired product shape.
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